HARDWARE / PRODUCT

Modified Low Power Stationary Plasma Thruster with 70 mm Diameter of the Accelerating Channel

Glavkosmos
Modified Low Power Stationary Plasma Thruster with 70 mm Diameter of the Accelerating Channel

In terms of discharge power it has been forced up to 1250 W. Propellant - xenon. Consists of the anode and cathode units. Classical scheme of the magnetic system of armored type with magnetic screens. Outside diameter of the accelerating channel is 70 mm. Mean diameter of the accelerating channel is

Technical specifications

Discharge power
660 W
Discharge voltage
300 V
Discharge current
2.2 A
Thrust
40 mN
Specific impulse
1500 s
Efficiency
48%
Specific power
275 W/kg
Power-to-thrust ratio
16.5 W/mN
Total impulse
> 1 MN∙s
Mass
2.4 kg

About

In terms of discharge power it has been forced up to 1250 W. Propellant – xenon. Consists of the anode and cathode units. Classical scheme of the magnetic system of armored type with magnetic screens. Outside diameter of the accelerating channel is 70 mm. Mean diameter of the accelerating channel is 55 mm. New structural materials and components. Manufacturing lead time is given without taking into account the time needed to procure materials (4 months) and procured parts and components (6 months).

Documentation

No public datasheet yet — request the datasheet / ICD from the supplier.

Source: trade.glavkosmos.com ↗